Export Control
EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.Copyright
© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).Applicability
V2500-A1
Common Information
TASK 72-45-20-440-002-A00 HPT Case And Vane Assembly - Final Assemble The Case And Vane Assembly, Assembly-002
General
Fig/item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the IPC.
For all parts identified in a different Chapter/Section/Subject, the applicable Chapter/Section/Subject comes before the Fig/item number.
For standard torque data and procedures, refer to SPM TASK 70-41-00-400-501 and SPM TASK 70-41-02-400-501.
Special torque data and assembly tolerances are included in the procedure.
Lubricate all threads and abutment faces of nuts and bolts with CoMat 10-077 APPROVED ENGINE OILS, unless other lubricants are referred to in the procedure.
To identify, lubricate and install seal rings, refer to SPM TASK 70-44-01-400-501.
The number for each radial location must be identified in a clockwise direction. These start at the engine top position when you look from the rear of the engine, unless stated differently in the procedure.
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Torque wrench, range 0 to 100 lbfin (0 to 11.298 Nm) | LOCAL | Torque Wrench 0 to 100 | ||
| IAE 1P16013 Fixture | 0AM53 | IAE 1P16013 | 1 | |
| IAE 1P16026 Assembly fixture | 0AM53 | IAE 1P16026 | 1 | |
| IAE 1P16159 Fixture | 0AM53 | IAE 1P16159 | 1 | |
| IAE 1P16173 Lift sling | 0AM53 | IAE 1P16173 | 1 | |
| IAE 1P16177 Marking plate | 0AM53 | IAE 1P16177 | 1 | |
| IAE 1P17012 Orientation ring | 0AM53 | IAE 1P17012 | 1 | |
| IAE 1P17016 Seating fixture | 0AM53 | IAE 1P17016 | 1 | |
| IAE 1P17756 Parallel measuring bar | 0AM53 | IAE 1P17756 | 1 | |
| IAE 1P17758 Protective cover | 0AM53 | IAE 1P17758 | 1 | |
| IAE 1P17771 Orientation adapter | 0AM53 | IAE 1P17771 | 19 | |
| IAE 1P17772 Socket | 0AM53 | IAE 1P17772 | 1 |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 01-573 WAX BLEND, PARAFFIN | 24269 | CoMat 01-573 | ||
| CoMat 02-141 LOCKWIRE | LOCAL | CoMat 02-141 | ||
| CoMat 10-029 CORROSION PREVENTIVESLUSHING OIL | 0AM53 | CoMat 10-029 | ||
| CoMat 10-077 APPROVED ENGINE OILS | X333X | CoMat 10-077 | ||
| CoMat 10-094 ANTI-SEIZE COMPOUND, PURE Ni-SPECIAL | K2147 | CoMat 10-094 | ||
| CoMat 10-129 ANTI-SEIZE PASTE | 34568 | CoMat 10-129 |
Safety Requirements
NONEProcedure
Refer to Figure.
Reference the interference at location 1510. If required use the data written as a note in TASK 72-45-21-200-001 and TASK 72-45-27-200-001-A00.
Table 1. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
REJECT IF
PART IDENT
Size
Clearance
(Select fit)
MORE THAN
LOCATION 1510
HP turbine case assembly
ENGINE-HP TURBINE CASE ASSEMBLY (72-45-21,01-010), bore
Stage 2 HPT support assembly
ENGINE-STAGE 2 HPT SUPPORT ASSEMBLY (72-45-27,01-010), location
Diameter
HP turbine case assembly
bore
28.583
Intf
28.583
Intf
28.577
0.002
28.577
0.002
Stage 2 HPT support assembly
28.591
0.014
28.591
0.014
location diameter
28.585
Intf
28.580
Intf
Table 2. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
REJECT IF
PART IDENT
Size
Clearance
(Select fit)
MORE THAN
LOCATION 1510
HP turbine case assembly
ENGINE-HP TURBINE CASE ASSEMBLY (72-45-21,01-010), bore
Stage 2 HPT support assembly
ENGINE-STAGE 2 HPT SUPPORT ASSEMBLY (72-45-27,01-010), location
diameter
HP turbine case assembly
bore
726.008
Intf
726.008
Intf
725.856
0.051
725.856
0.051
Stage 2 HPT support assembly
726.211
0.356
726.211
0.356
location diameter
726.059
Intf
725.932
Intf
SUBTASK 72-45-20-220-146 Reference the Fits and Clearances of the HP Turbine Case and Vane Assembly at Location 1510
Refer to Figure.
Reference clearance at location 1512. If required use the data written as a note in TASK 72-45-00-200-001 and TASK 72-45-24-200-001.
Table 3. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
REJECT IF
PART IDENT
Size
Clearance
(Non-Select)
MORE THAN
LOCATION 1512
Instrumentation plug
ENGINE-HP TURBINE ROTOR AND STATOR ASSEMBLY (72-45-00,01-140), location
diameter
Stage 2 HPT ring segment and
vane cluster assembly
(72-45-24,02-270 thru
02-290), location
diameter
Instrumentation plug
location diameter
0.498
Clear
0.503
0.001
Stage 2 HPT ring segment
0.504
0.012
and vane cluster assembly
0.510
Clear
location diameter
Table 4. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
REJECT IF
PART IDENT
Size
Clearance
(Non-Select)
MORE THAN
LOCATION 1512
Instrumentation plug
ENGINE-HP TURBINE ROTOR AND STATOR ASSEMBLY (72-45-00,01-140),
location diameter
Stage 2 HPT ring segment
and vane cluster assembly
(72-45-24,02-270 thru
02-290), location
diameter
Instrumentation plug
location diameter
12.649
Clear
12.776
0.025
Stage 2 band segment and
12.802
0.305
vane cluster assembly
12.954
Clear
location diameter
SUBTASK 72-45-20-220-147 Reference Fits and Clearances of the HP Turbine Case and Vane Assembly at Location 1512
Refer to Figure.
Reference clearance at location 1513. If required use the data written as a note in TASK 72-45-00-200-001 and TASK 72-45-21-200-001.
Table 5. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
REJECT IF
PART IDENT
Size
Clearance
(Non-Select)
MORE THAN
LOCATION 1513
Instrumentation plug
ENGINE-HP TURBINE ROTOR AND STATOR ASSEMBLY (72-45-00,01-140), location
diameter
HP turbine case assembly
ENGINE-HP TURBINE CASE ASSEMBLY (72-45-21,01-010), location
diameter
Instrumentation plug
location diameter
0.733
Clear
0.743
0.002
HP turbine case assembly
0.745
0.022
location diameter
0.755
Clear
Table 6. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
REJECT IF
PART IDENT
Size
Clearance
(Non-Select)
MORE THAN
LOCATION 1513
Instrumentation plug
ENGINE-HP TURBINE ROTOR AND STATOR ASSEMBLY (72-45-00,01-140),
location diameter
HP turbine case assembly
ENGINE-HP TURBINE CASE ASSEMBLY (72-45-21,01-010), location
diameter
Instrumentation plug
location diameter
18.618
Clear
18.872
0.051
HP turbine case assembly
18.923
0.559
location diameter
19.177
Clear
SUBTASK 72-45-20-220-148 Reference Fits and Clearances of the HP Turbine Case and Vane Assembly at Location 1513
Refer to Figure.
Put the IAE 1P16177 Marking plate 1 off on a work bench.
Mark the identification numbers 1 thru 19 and the mating number between the two rivets on the vane assemblies. Use the vibration peen method. Refer to SPM TASK 70-09-00-400-501.
Put the 17 Stage 2 HPT ring segment and vane cluster assemblies ENGINE-STAGE 2 HPT RING SEGMENT AND VANE CLUSTER (72-45-24,02-050) and two Stage 2 HPT ring segment and vane cluster assemblies ENGINE-STAGE 2 HPT RING SEGMENT AND VANE CLUSTER (72-45-24,02-260) on the marking plate with the leading edge down.
SUBTASK 72-45-20-440-148 Put the Stage 2 HPT Ring Segment and Vane Cluster Assemblies on the Marking Plate
Refer to Figure.
Install a seal assembly ENGINE-STAGE 2 HPT RING SEGMENT AND VANE CLUSTER (72-45-24, 02-190) into the slot with the longer leg parallel to the outer vane platform and the short leg in the slot adjacent to the anti-rotation lug on the vane.
Install a seal ENGINE-STAGE 2 HPT RING SEGMENT AND VANE CLUSTER (72-45-24, 02-200) into the slot that remains on the outer vane platform.
Install a seal ENGINE-STAGE 2 HPT RING SEGMENT AND VANE CLUSTER (72-45-24, 02-200) in between the clustered vanes.
Install a seal ENGINE-STAGE 2 HPT RING SEGMENT AND VANE CLUSTER (72-45-24, 02-220) into the slot of the ring segment.
Install a seal ENGINE-STAGE 2 HPT RING SEGMENT AND VANE CLUSTER (72-45-24, 02-180) into the slot of the outer vane platform with the short leg of the seal to the ring segment.
Install the seals and seal assembly by the procedures given below. Put the seals in the slots located on the right side of the 19 vane assemblies. Use CoMat 01-573 WAX BLEND, PARAFFIN to hold in position. Remove the wax that is not necessary at all locations.
SUBTASK 72-45-20-440-149 Install the Seals and the Seal Assembly in the Stage 2 HPT Ring Segment and Vane Cluster Assembly Slots
Refer to Figure.
Install a standard two cable sling to the IAE 1P16026 Assembly fixture 1 off. Attach the sling to a hoist and position the fixture on a work bench with the legs down. Remove the sling and hoist.
Carefully align the seals in the number two vane with the seal slots in the number one vane and engage the seals. Make sure no damage occurs to the seals.
NOTE
When you install the vane assemblies, the adjacent vane assemblies can be moved out to engage the seals correctly.
Make sure the two vane assemblies with the instrumentation holes are at the location on the fixture that is identified as borescope.
Install the vane assembly, identified as number two in a clockwise direction when you look down from the rear of the fixture.
Install the vane assemblies that remain, by number, in a clockwise direction by the procedure given in Step.
Install the Stage 2 HPT ring segment and vane cluster assemblies in the fixture.
SUBTASK 72-45-20-440-150 Install the Stage 2 HPT Ring Segment and Vane Cluster Assemblies in the Fixture
Refer to Figure.
Install the gasket ENGINE-STAGE 2 HPT RING SEGMENT AND VANE CLUSTER (72-45-24,02-020) in the outer groove of the Stage 2 HPT ring segment and vane cluster assemblies.
Install the IAE 1P16173 Lift sling 1 off to the front flange of the turbine case assembly (flange with the dowel pin) and attach with the washers and nuts.
SUBTASK 72-45-20-440-151 Install the HP Turbine Case Assembly
Install the gasket ENGINE-STAGE 2 HPT RING SEGMENT AND VANE CLUSTER (72-45-24,02-010) in the inner groove of the Stage 2 ring segment and vane cluster assemblies, Figure.
Install the Stage 1 HPT band segment ENGINE-STAGE 1 HPT DUCT SEGMENT (72-45-23,01-040) in the groove of the vane assemblies with the large outer diameter down.
Install the two Stage 1 HPT band segments ENGINE-STAGE 1 HPT DUCT SEGMENT (72-45-23,01-020) in the groove of the vane assemblies. Make sure the band segments do not go over each other.
Install the Stage 1 HPT band segments.
Install one IAE 1P17771 Orientation adapter 19 off on the inner flange of the case assembly adjacent to the two installed duct segments.
NOTE
The orientation adapter shows the relative position of the duct segments to the bolthole in the case.Install the duct segments that remain in a clockwise direction by the procedures given in Step.
Install the Stage 1 HPT duct segment assemblies ENGINE-STAGE 1 HPT DUCT SEGMENT (72-45-23,01-060).
Install the Stage 1 HPT duct seal ENGINE-STAGE 1 HPT DUCT SEGMENT (72-45-23, 01-080) between each of the duct segments.
Use CoMat 01-573 WAX BLEND, PARAFFIN to hold the seal in position.
Install a Stage 1 HPT duct support seal (75-45-22, 01-060) in the recess slot located on the right side of each duct support. Put the short side of the seal in the slot, Figure.
Apply CoMat 10-094 ANTI-SEIZE COMPOUND, PURE Ni-SPECIAL or CoMat 10-029 CORROSION PREVENTIVESLUSHING OIL to the threads of the bolts ENGINE-STAGE 1 HPT DUCT SUPPORT SET (72-45-22, 01-100).
Install the duct supports that remain in a clockwise direction by the procedures given in Step.
Torque the bolts 180 degrees apart to 62 to 72 lbfin (7.005 to 8.135 Nm). Use the IAE 1P17772 Socket 1 off.
NOTE
This is the distance from the front flange of the case assembly to inner diameter front surface of each Stage 1 duct support.Measure the distance at Dimension D at 19 locations. Use the IAE 1P17756 Parallel measuring bar 1 off and a depth micrometer.
Measure the distance at Dimension D.
Install the Stage 1 HPT duct supports ENGINE-STAGE 1 HPT DUCT SUPPORT SET (72-45-22, 01-010).
SUBTASK 72-45-20-440-152 Identify the Stage 1 HPT Band Segments, Stage 1 HPT Duct Segment Assemblies and Stage 1 HPT Duct Supports
Refer to Figure.
SUBTASK 72-45-20-440-153 Turn the HP Turbine Case Assembly
Install the gasket ENGINE-STAGE 2 HPT DUCT SEGMENT (72-45-25, 01-010) in the inner diameter groove of the Stage 2 ring segment and vane cluster assemblies, Figure.
Install the Stage 2 HPT band segment assembly ENGINE-STAGE 2 HPT DUCT SEGMENT (72-45-25, 01-040) in the vane assembly groove with the cooling air holes down.
Install the two Stage 2 HPT band segment assemblies ENGINE-STAGE 2 HPT DUCT SEGMENT (72-45-25, 01-020) in the vane assembly groove in a clockwise direction. Position the tab end of the band segment to the outer side of the adjacent segments.
Install the Stage 2 HPT band segment assemblies.
Use CoMat 01-573 WAX BLEND, PARAFFIN to hold the seal in position.
Install a stage 2 HPT duct seal ENGINE-STAGE 2 HPT DUCT SEGMENT (72-45-25, 01-080) in the recess slot on the right side of each duct segment. Position the short 90 degree end of the seal in the slot of the duct segment lug.
Install the duct segment in the vane assembly groove and on the inner side of the band segment. Align the center of the duct segment with the center of the first band segment at the 12 o'clock position.
NOTE
The convex side of the inner diameter of the band segment must align with the cavity on the outer diameter of the duct segment.
Install the stage 2 HPT duct segments.
Install the IAE 1P17012 Orientation ring 1 off, Figure.
Install the gasket ENGINE-SECOND STAGE HPT DUCT SUPPORT (72-45-26,01-010) in the slot of the Stage 2 HPT duct segment assemblies.
SUBTASK 72-45-20-440-154 Install the Stage 2 HPT Band Segment Assemblies and the Stage 2 Duct Segments in the Turbine Case Assembly
Refer to Figure.
Attach a standard three cable sling to the three lifting eyes on the IAE 1P17016 Seating fixture 1 off.
Install the Stage 2 HPT seal ENGINE-STAGE 2 HPT SUPPORT ASSEMBLY (72-45-27, 01-060) in the inner diameter of the fixture with the outer diameter of the seal down.
Install the Stage 2 HPT support assembly ENGINE-STAGE 2 HPT SUPPORT ASSEMBLY (72-45-27, 01-010) with the tapered outer diameter down and align the dowel pin in the fixture with the dowel hole in the support assembly flange.
Use CoMat 01-573 WAX BLEND, PARAFFIN to hold the seal in position.
Install a Stage 2 HPT duct support seal ENGINE-SECOND STAGE HPT DUCT SUPPORT (72-45-26, 01-060) in the slot on the right side of each duct support assembly. Engage the short side of the seal in the recess slot.
Do Step again until all the duct support assemblies are seated in the duct support assembly.
Seat the Stage 2 HPT duct support assemblies in the stage 2 HPT support assembly.
NOTE
The duct support assemblies must be seated equally.
Install the Stage 2 HPT duct support assemblies ENGINE-SECOND STAGE HPT DUCT SUPPORT (72-45-26, 01-020).
SUBTASK 72-45-20-440-155 Assemble the Stage 2 HPT Seal, Stage 2 HPT Duct Support Assemblies and Stage 2 HPT Support Assembly in the Seating Fixture
Remove the nuts and screws that attach the orientation ring to the rear flange of the turbine case assembly, Figure.
Install the assembled Stage 2 HPT seal, Stage 2 duct support assemblies and Stage 2 HPT support assembly in the IAE 1P16013 Fixture 1 off, Figure.
Install the fixture and assembled seal, duct support and support on the rear flange of the turbine case assembly, Figure.
Apply CoMat 10-094 ANTI-SEIZE COMPOUND, PURE Ni-SPECIAL or CoMat 10-129 ANTI-SEIZE PASTE to the threads of the eight screws ENGINE-STAGE 2 HPT SUPPORT ASSEMBLY (72-45-27,01-040).
Install the screws in the eight chamfered holes in the support assembly. Torque the screws to 23 to 26 lbfin (2.599 to 2.938 Nm).
NOTE
This is the distance from the rear surface of the Stage 2 support assembly flange to each of the rear surfaces of the Stage 2 HPT duct support assemblies. This will make sure all the parts are fully engaged.
Attach the Stage 2 HPT support assembly to the turbine case assembly flange.
Measure the distance at Dimension F at 19 locations. Use the IAE 1P17756 Parallel measuring bar 1 off and a depth micrometer.
Measure the distance at Dimension F, Figure.
Examine the clearance at Dimension E between the 38 Stage 1 duct segments, Figure.
SUBTASK 72-45-20-440-156 Install the Assembled Stage 2 HPT Seal, Stage 2 HPT Duct Support Assemblies and Stage 2 HPT Support Assembly
Install the gaskets ENGINE-HP TURBINE ROTOR AND STATOR ASSEMBLY (72-45-00,01-120) in the two borescope bosses on the turbine case assembly.
Install the instrumentation plugs ENGINE-HP TURBINE ROTOR AND STATOR ASSEMBLY (72-45-00,01-140) in the two borescope bosses.
Install the two retaining bolts ENGINE-HP TURBINE ROTOR AND STATOR ASSEMBLY (72-45-00,01-160) that attach the instrumentation plug at each location.
Torque the bolts to 65 to 85 lbfin (7.344 to 9.604 Nm). Safety the bolts with CoMat 02-141 LOCKWIRE.
SUBTASK 72-45-20-440-157 Install the Instrumentation Plugs
Refer to Figure.
Install the bolts ENGINE-HP TURBINE ROTOR AND STATOR ASSEMBLY (72-45-00,01-220) through the plate and bracket and attach them with the nuts ENGINE-HP TURBINE ROTOR AND STATOR ASSEMBLY (72-45-00,01-200).
If necessary, install the HPT rotor and stator identification plate ENGINE-HP TURBINE ROTOR AND STATOR ASSEMBLY (72-45-00,01-240) to the bracket on the front flange of the turbine case assembly.
SUBTASK 72-45-20-440-158 Install the HPT Rotor and Stator Identification Plate
Refer to Figure.
Install the IAE 1P16173 Lift sling 1 off to the rear flange of the turbine case assembly (flange with the dowel pin) and attach with the washers and nuts.
Install the IAE 1P17758 Protective cover 1 off on the rear flange of the case and vane assembly.
SUBTASK 72-45-20-440-159 Put the HP Turbine Case and Vane Assembly on a Pallet
Figure: HP Turbine Case and Vane Assembly Fits and Clearances
HP Turbine Case and Vane Assembly Fits and Clearances

Figure: Stage 2 HPT Ring Segment and Vane Cluster Assembly Identification
Stage 2 HPT Ring Segment and Vane Cluster Assembly Identification

Figure: Install the Seals and Seal Assembly in the Ring Segment and Vane Cluster Assembly
Install the Seals and Seal Assembly in the Ring Segment and Vane Cluster Assembly

Figure: Stage 2 HPT Ring Segment and Vane Cluster Assemblies in the Fixture
Stage 2 HPT Ring Segment and Vane Cluster Assemblies in the Fixture

Figure: Install the HP Turbine Case Assembly
Install the HP Turbine Case Assembly

Figure: Stage 1 HPT Band Segments Identification
Stage 1 HPT Band Segments Identification

Figure: Stage 1 HPT Duct Segment Assemblies Identification
Stage 1 HPT Duct Segment Assemblies Identification

Figure: Stage 1 HPT Duct Supports Identification
Stage 1 HPT Duct Supports Identification

Figure: Install the Stage 1 HPT Duct Segment Assemblies and the Stage 1 HPT Band Segments
Install the Stage 1 HPT Duct Segment Assemblies and the Stage 1 HPT Band Segments

Figure: Install the Stage 1 HPT Duct Supports
Install the Stage 1 HPT Duct Supports

Figure: Remove the IAE 1P16026 Assembly Fixture
Remove the IAE 1P16026 Assembly Fixture

Figure: Install the Stage 2 HPT Duct Segments and the Stage 2 HPT Band Segment Assemblies
Install the Stage 2 HPT Duct Segments and the Stage 2 HPT Band Segment Assemblies

Figure: Stage 2 HPT Band Segment and Stage 2 HPT Duct Segments
Stage 2 HPT Band Segment and Stage 2 HPT Duct Segments

Figure: Assemble the Stage 2 HPT Duct Support Assembly, Stage 2 HPT Duct Support Assemblies and Stage 2 HPT Seal
Assemble the Stage 2 HPT Duct Support Assembly, Stage 2 HPT Duct Support Assemblies and Stage 2 HPT Seal

Figure: Stage 2 HPT Support Assembly, Stage 2 HPT Duct Support Assemblies and Stage 2 HPT Seal in the Fixture
Stage 2 HPT Support Assembly, Stage 2 HPT Duct Support Assemblies and Stage 2 HPT Seal in the Fixture

Figure: Stage 2 HPT Support Assembly, Stage 2 HPT Duct Support Assembly and Stage 2 HPT Seal Installation
Stage 2 HPT Support Assembly, Stage 2 HPT Duct Support Assembly and Stage 2 HPT Seal Installation

Figure: Install the Instrumentation Plugs
Install the Instrumentation Plugs

Figure: HPT Rotor and Stator Identification Plate Installation
HPT Rotor and Stator Identification Plate Installation

Figure: Put the HP Turbine Case and Vane Assembly on a Pallet
Put the HP Turbine Case and Vane Assembly on a Pallet

